SBIR/STTR Research Award

Spray Protection for Landing on Aluminum Ships

Award identifier 18d2b66fb0245f15ffe943351c3f6025d63925ca436eee02a5f11e25e63b2731Awarding agency Department of Defense · Navy

Award amount

$999,289

Program and phase

SBIR · Phase II

Award year

2021

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Award details

Awarding agency
Department of Defense
Branch
Navy
Recipient company
CELLULAR MATERIALS INTERNATIONAL, INC.
Proposal award date
2021-01-15
Contract end date
2023-01-13
UEI
UXMNC56MVY75
Solicitation number
19.2
Topic code
N192-127

Research abstract

The proposed program seeks to continue the development of a novel spray cooling thermal management system that protects aluminum flight decks from the thermal impact of MV-22 operations. The MV-22 Osprey aircraft is a critical asset for the Navy that is seeing expanded operational roles in military and humanitarian missions. Operations on amphibious warfare and other Navy ships have led to concerns about the thermomechanical effects in the flight deck from exhaust plume impingement. Research programs under ONR and DARPA sponsorships have sought protection solutions to be retrofit onto steel flight decks (LHA/LHD and LSD). At MV-22 exhaust plume temperatures, flight decks constructed from aluminum alloy suffer material degradation in addition to excessive thermally induced stresses and presents a unique challenge. The proposed spray cooling system – named SPLASH (Spray Protection for Landing on Aluminum SHips) – uses synthetic coolant spray to efficiently absorb and remove heat from the flight deck. The concept uses an array of nozzles positioned within the corrugated channels of the existing deck extrusion to direct coolant spray onto the underside of the top face. Flight Deck Tie Downs are spray cooled from underneath by a contained nozzle assembly mounted below each component. The system is designed to operate completely below the deck’s top surface so that the risk to flight deck operations and personnel are reduced or eliminated. Previous analysis shows the capability of this system to maintain flight deck temperatures below the objective requirement for deck planking (212°F/100°C) and Flight Deck Tie Downs (149°F/65°C), when subjected to MV-22 nacelle exhaust. The proposed work will develop and demonstrate all “in-the-deck” system components under simulated MV-22 thermal loading at intermediate-scale (Base period) and develop the full cooling loop and system design (Option period).  A successful program will demonstrate the ability of the SPLASH system to meet Navy objectives for unmitigated MV-22 operations on aluminum flight decks and develop full system designs ready for large-scale fabrication and testing in Phase III.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

16 SBIR/STTR records share this UEI (2002–2021). Reported award amounts total $4,362,262. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Science Foundation, Department of Homeland Security, National Aeronautics and Space Administration

Agency intelligence

Department of Defense

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